This page presents the S-N curves and fatigue limit of CX steel samples that underwent shot-peening only, obtained using the bending tests of rotating bars with AM layers normal to the axis of rotation.
Build orientation of longitudinal axis | vertical |
---|---|
Position with respect to inert gas flow | undefined |
Post-processing | shot-peening |
Fatigue limit (MPa) | 123 |
---|---|
Number of cycles to failure N | N=2,81⋅109⋅S-1,77 |
Stress amplitude S (MPa) | S=218241⋅N-0,565 |
Explanation of the terms are given at the page Fatigue strength description.
This page is a part of the section DMLS/SLM: Fatigue design rules.